View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 00053U 26041.24721185 +.00000000 +00000-0 +38327-3 0 00000
2 00053 47.2796 13.9085 0098130 59.7762 301.2701 12.17401186 03
| Epoch (UTC): | 10 February 2026 05:55:59 |
| Eccentricity: | 0.0098130 |
| inclination: | 47.2796° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 13.9085° |
| argument of perigee: | 59.7762° |
| revolutions per day: | 12.17401186 |
| mean anomaly at epoch: | 301.2701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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